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Zainul Huda

Researcher at University of Malaya

Publications -  38
Citations -  733

Zainul Huda is an academic researcher from University of Malaya. The author has contributed to research in topics: Alloy & Grain growth. The author has an hindex of 12, co-authored 35 publications receiving 598 citations. Previous affiliations of Zainul Huda include King Saud University & Majmaah University.

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Materials selection in design of structures and engines of supersonic aircrafts: A review

TL;DR: In this article, the advances in the materials selection for applications in structures and engines of current and future supersonic aircrafts are reviewed, and a new materials selection chart is presented that would enable aerospace designers to select appropriate materials for application in high-performance current and hypersonic aircraft.
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Characterization of 2024-T3: An aerospace aluminum alloy

TL;DR: In this paper, the authors used an optical microscope linked with a computerized imaging system using MSQ software to detect three types of inclusions: Al−Cu, Al-Cu-Fe, Al−Fe-Fe-Si−Mn, and Al−Si-Mn enriched regions.
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A comparative analysis of tensile and impact-toughness behavior of cold-worked and annealed 7075 aluminum alloy

TL;DR: In this article, a comparative analysis of effects of cold working (CW) and annealing on tensile and impact-toughness behavior of 7075 Al alloy was performed. And it was found that cold rolling has a significant effect on decreasing the impact toughness of alloy that enhance with amount of CW; this loss in impact energy could not be compensated by recrystallization process.
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Metallurgical failure analysis for a blade failed in a gas-turbine engine of a power plant

TL;DR: In this paper, the failed gas-turbine blades (first stage blades) were acquired from TNB Research Sdn. Bhd: a subsidiary of Malaysian power-generation industry (TNB, Malaysia).
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Development of Heat Treatment Process for a P/M Superalloy for Turbine Blades

TL;DR: In this article, a powder metallurgy (P/M) superalloy turbine blades are increasingly being used in jet-aircraft engines, and the improvement in creep strength is ensured though microstructural control achieved by developing a suitable heat treatment process.